US4200784A - Hollow shaft bore heater assembly - Google Patents

Hollow shaft bore heater assembly Download PDF

Info

Publication number
US4200784A
US4200784A US05/857,481 US85748177A US4200784A US 4200784 A US4200784 A US 4200784A US 85748177 A US85748177 A US 85748177A US 4200784 A US4200784 A US 4200784A
Authority
US
United States
Prior art keywords
shaft
slots
heater assembly
shaft bore
foundation members
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US05/857,481
Inventor
Jacques E. Albaric
Forrest E. Coyle
Thomas P. Sherlock
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Priority to US05/857,481 priority Critical patent/US4200784A/en
Priority to IT30255/78A priority patent/IT1100599B/en
Priority to JP14975478A priority patent/JPS5486828A/en
Application granted granted Critical
Publication of US4200784A publication Critical patent/US4200784A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00Ohmic-resistance heating
    • H05B3/0095Heating devices in the form of rollers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • F01D25/10Heating, e.g. warming-up before starting

Definitions

  • This invention relates to hollow shafts of turbines, and more particularly, to means for heating the hollow shaft from its inside to its outside.
  • Such spinning reserve requires capital expenditures for additional equipment and often results in high operating costs for that equipment due to its relatively low efficiency at partload, normal demand operation. Reduction in the amount of spinning reserve necessitates having the capability of quickly accelerating steam turbines from turning gear operation to operating speed while avoiding high internal material stresses during such fast rotative acceleration and material temperature elevation.
  • U.S. Pat. No. 2,004,777 which issued June 11, 1935, discloses electrical heating of turbine casings and other associated stationary parts such as flanges.
  • U.S. Pat. No. 1,811,383 which issued June 23, 1931, illustrates a system for preheating turbine components by continuously passing heating steam therethrough and removal of moisture droplets condensed within the turbine.
  • Both of the aforementioned patents illustrate prior attempts to reduce turbine startup time by preheating selected parts of the turbine.
  • Neither patent, however, illustrates heating the turbine shaft from the inside toward the outside. It can be shown that the shaft material near the bore experiences the highest centrifugal force stress loading and neither of the aforementioned patents provide means for directly heating the material in such region.
  • a shaft bore heater assembly for heating a hollow shaft from its inside surface.
  • the invention generally comprises a hollow, rotatable shaft which has a plurality of foundation members disposed inside, a plurality of electrical heaters disposed in open-mouth slots formed in the heater foundation members, means for restraining the heaters in those slots, and means for biasing the foundation member's outer surfaces into engagement with the shaft's inside surface.
  • a preferred embodiment of the invention includes heater foundation members which, when assembled, form a substantially cylindrical structure with the biasing means being disposed between circumferentially adjacent foundation members. Insulation attached to the inner surface of the foundation members promotes heat flux in the radially outward direction and acts to restrain the heaters within the slots by covering the slots' open mouths.
  • the biasing means are restrained in biasing position by disposing portions thereof in indentations formed on circumferential ends of circumferentially adjacent foundation members wherein the biasing means induce engagement between foundation members and the shaft.
  • the heater foundation member's slots are equally spaced in the circumferential direction and axially disposed to provide uniform heating of the shaft.
  • FIG. 1 is a partial transverse sectional view of a schematized turbine
  • FIG. 2 is a partial sectional view of the turbine's electrical supply flange
  • FIG. 3 is a sectional end view of a portion of the present invention.
  • the present invention is concerned primarily with heating means for the inside of hollow, rotatable shafts. Accordingly, in the description which follows the invention is shown embodied in a large steam turbine. It should be understood, however, that the invention may be utilized as a heating means for a rotatable hollow shaft in any device.
  • FIG. 1 schematically illustrates steam turbine 10 which is illustrated as being a double axial flow turbine.
  • Generator end flange 12 and governor end flange 14 are situated on opposite axial ends of heat conductive turbine shaft 16 which is journaled between bearings 18 and 20.
  • Shaft 16 is seen to be hollow with an inner surface 16a and outer surface 16b.
  • shaft heater assembly 22 Situated within shaft surface 16a is shaft heater assembly 22 better illustrated in FIG. 3.
  • Shaft heater assembly 22 constitutes two half cylinder heater foundation members which are made of a material identical to or of the same nature as shaft 16.
  • Heater foundations 24 and 26 have axially extending slots 28 formed on their radially inner surfaces 30 with the slots' mouths opening radially towards shaft 16's axis of rotation and with the slot's bottoms being disposed within the foundations.
  • Tubular electric heaters 32, 34, 36, 38, 40, and 42 are distributed in slots 28 with their heating coils extending axially between the turbine's gland seals (not shown) normally situated at positions 44 and 48.
  • the electrical heater's conductive elements while shown schematically in FIG. 1, are electrically insulated from the foundation members 24 and 26. Insulation 50 is attached to inner surface 30 of heater foundations 24 and 26 and extends across the open mouths of the axially extending slots so as to restrain heaters 32 through 42 and spacers 49 therein during non-rotation of shaft 16.
  • Spacers 49 illustrated in FIGS. 2 and 3, are shaped to cooperate with the tubular heaters and prevent penetration thereinto by biasing means such as wavy bias or leaf springs 51.
  • Springs 51 are disposed between insulation 50 and spacers 49 to urge the electric heaters against the bottoms of their slots. Spring 51 for urging heater 34 was deleted for purposes of clarity.
  • Biasing means such as springs or Bellville washers 52 are disposed in cooperating indentations 54 and 56 formed on circumferentially adjacent ends of foundation members 24 and 26 respectively. Indentations 54 and 56 restrain springs 52 within a relatively small radial distance as illustrated in FIG. 3 and a relatively small axial distance as illustrated in FIG. 2.
  • Springs 52 and 54 permit the shaft bore heater assembly to be inserted and removed from shaft 16 with relative ease while maintaining good heat transfer contact between inner shaft surface 16b and both outer surfaces 58 and 60 of foundation members 24 and 26, respectively, during relatively slow shaft rotation or rest.
  • FIG. 2 is a partial transverse sectional view of electrical input generator flange 12 and its connection with heaters 34 and 40.
  • heaters 40 and 34 are illustrated in their non-heating and heating positions respectively.
  • heater 34 is elongated in the axial direction due to thermal expansion from heat generated by that heater.
  • Double rings 62, 64, 66, 68, 70, and 72 are illustrated along the outer periphery of flange 12.
  • Conducting studs extending radially through flange 12 from inner rings 64, 68, and 72 provide electrical energy through flexible or braided connectors to the electrical heaters which constitute a portion of the present invention.
  • the details of such double slip-ring construction are set forth in copending application Ser. No. 857,480, filed Dec. 5, 1977.
  • slip ring pair 62 and 64 For illustrative purposes here, only copper stud 74 connecting slip ring pair 62 and 64 is shown in operating position providing electrical energy to heater 40 through flexible or braided conducting connector 76. Each pair of slip rings is connected to two heaters. The preferred embodiment has three-phase power supplied to the illustrated six heaters which are wired in delta.
  • delta wiring from a three-phase power supply to six electrical heaters has been indicated as preferred, it is to be understood that any number of electrical heaters may be utilized with any comparable single or multiphase power supply system and those heaters may be electrically wired in "Y" as well.
  • any number of heater foundation members may be utilized to form the preferred, assembled cylindrical shape since the invention is not to be limited to dual semi-cylindrical foundation members.

Abstract

A hollow, rotatable shaft bore heater assembly for heating a shaft from its inside to its outside. Rapid rotatable shaft heating is provided by a plurality of electrical heaters situated in slots formed on the inner surfaces of a plurality of foundation members which are insertable in the hollow shaft and are biased thereagainst by biasing structure. When assembled, the foundation members constitute a substantially cylindrical structure which has the slots formed on its inner surface and the electrical heaters are restrained within those axially extending and circumferentially separated slots by insulation disposed on the inner surface of the foundation members across the slots open mouths. The biasing structure provides biasing force between circumferentially adjacent foundation members so as to maintain contact between the shaft and foundation members during non-rotation of the shaft.

Description

BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates to hollow shafts of turbines, and more particularly, to means for heating the hollow shaft from its inside to its outside.
2. Description of the Prior Art
When large rotating apparatus such as steam turbines which normally operate at elevated temperatures are removed from service, access to the turbine by the steam or other heating medium is usually prevented and the turbine is either brought to rest or rotated at low RPM's by turning gears. To safely and reliably accelerate the steam turbine to synchronous speed and bring it under load, the turbine parts which are normally exposed to the hot, motive steam must be increased in temperature at a relatively slow rate to avoid high internal material stresses from being experienced. Such slow temperature increases are especially critical for the turbine's shaft since, in addition to the high thermal stresses experienced by it, high, centrifugally induced stresses are imposed upon it. To assure quick response to increasing load demand it has often been necessary for utilities to maintain an abnormally high spinning reserve of generating capacity. Such spinning reserve requires capital expenditures for additional equipment and often results in high operating costs for that equipment due to its relatively low efficiency at partload, normal demand operation. Reduction in the amount of spinning reserve necessitates having the capability of quickly accelerating steam turbines from turning gear operation to operating speed while avoiding high internal material stresses during such fast rotative acceleration and material temperature elevation.
U.S. Pat. No. 2,004,777 which issued June 11, 1935, discloses electrical heating of turbine casings and other associated stationary parts such as flanges. U.S. Pat. No. 1,811,383 which issued June 23, 1931, illustrates a system for preheating turbine components by continuously passing heating steam therethrough and removal of moisture droplets condensed within the turbine. Both of the aforementioned patents illustrate prior attempts to reduce turbine startup time by preheating selected parts of the turbine. Neither patent, however, illustrates heating the turbine shaft from the inside toward the outside. It can be shown that the shaft material near the bore experiences the highest centrifugal force stress loading and neither of the aforementioned patents provide means for directly heating the material in such region. Further attempts to heat turbine shafts from their inside include routing heating steam to the inside bore, but it has been found that such practice can promote stress corrosion cracking of the turbine shaft and is thus considered undesirable. It is to be noted that U.S. Pat. No. 2,004,777 illustrates electrical heating of the casing elements only and provides no means for preheating the rotatable shaft element. A further disadvantage of U.S. Pat. No. 1,811,383 is that it requires a continuous steam flow through the turbine to maintain the desirable temperature in all turbine parts. Such practice is expensive since it requires constant expenditure of heat energy to maintain turbine component temperatures at acceptable levels.
Supplying electrical energy to electrical heaters disposed within turbine shafts has heretofore presented a variety of problems. Ser. No. 857,480, filed Dec. 5, 1977, provides a solution to many of the problems that previously existed for conducting electricity from a stationary source to the turbine shaft's interior. Since such conduction is now practical, it is desirable to obtain an electrical turbine bore heating system which uses relatively simple electrical heaters which can be easily assembled in turbine shafts, will provide uniform heating, and will have heating capability sufficient to rapidly heat the turbine shaft from its interior.
SUMMARY OF THE INVENTION
In accordance with the present invention a shaft bore heater assembly is provided for heating a hollow shaft from its inside surface. The invention generally comprises a hollow, rotatable shaft which has a plurality of foundation members disposed inside, a plurality of electrical heaters disposed in open-mouth slots formed in the heater foundation members, means for restraining the heaters in those slots, and means for biasing the foundation member's outer surfaces into engagement with the shaft's inside surface.
A preferred embodiment of the invention includes heater foundation members which, when assembled, form a substantially cylindrical structure with the biasing means being disposed between circumferentially adjacent foundation members. Insulation attached to the inner surface of the foundation members promotes heat flux in the radially outward direction and acts to restrain the heaters within the slots by covering the slots' open mouths. The biasing means are restrained in biasing position by disposing portions thereof in indentations formed on circumferential ends of circumferentially adjacent foundation members wherein the biasing means induce engagement between foundation members and the shaft. The heater foundation member's slots are equally spaced in the circumferential direction and axially disposed to provide uniform heating of the shaft.
Electrical heating of the shaft from the shaft's inside to a temperature at or above the shaft's brittle to ductile transition temperature permits fast rotative acceleration of the turbine from low temperature, low speed operation to its normal, elevated operating speed and temperature while avoiding the possibility of catastrophic mechanical failure due to excessive internal stresses. Since the shaft material near the bore experiences the highest stresses under centrifugal loading, heating the shaft from its bore minimizes thermal stresses in that location and thus permits higher rotative acceleration than has heretofore been possible. Heating the shaft from its bore also reduces thermal stresses at the shaft's outer periphery since that outer periphery is normally cold when it is exposed to relatively hot, motive steam during incremental loading of the turbine.
BRIEF DESCRIPTION OF THE DRAWINGS
The invention will be more fully understood from the following detailed description of a preferred embodiment taken in connection with the accompanying drawings, in which:
FIG. 1 is a partial transverse sectional view of a schematized turbine;
FIG. 2 is a partial sectional view of the turbine's electrical supply flange; and
FIG. 3 is a sectional end view of a portion of the present invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT
The present invention is concerned primarily with heating means for the inside of hollow, rotatable shafts. Accordingly, in the description which follows the invention is shown embodied in a large steam turbine. It should be understood, however, that the invention may be utilized as a heating means for a rotatable hollow shaft in any device.
FIG. 1 schematically illustrates steam turbine 10 which is illustrated as being a double axial flow turbine. Generator end flange 12 and governor end flange 14 are situated on opposite axial ends of heat conductive turbine shaft 16 which is journaled between bearings 18 and 20. Shaft 16 is seen to be hollow with an inner surface 16a and outer surface 16b. Situated within shaft surface 16a is shaft heater assembly 22 better illustrated in FIG. 3. Shaft heater assembly 22 constitutes two half cylinder heater foundation members which are made of a material identical to or of the same nature as shaft 16. Heater foundations 24 and 26 have axially extending slots 28 formed on their radially inner surfaces 30 with the slots' mouths opening radially towards shaft 16's axis of rotation and with the slot's bottoms being disposed within the foundations. Tubular electric heaters 32, 34, 36, 38, 40, and 42 are distributed in slots 28 with their heating coils extending axially between the turbine's gland seals (not shown) normally situated at positions 44 and 48. The electrical heater's conductive elements, while shown schematically in FIG. 1, are electrically insulated from the foundation members 24 and 26. Insulation 50 is attached to inner surface 30 of heater foundations 24 and 26 and extends across the open mouths of the axially extending slots so as to restrain heaters 32 through 42 and spacers 49 therein during non-rotation of shaft 16. Spacers 49, illustrated in FIGS. 2 and 3, are shaped to cooperate with the tubular heaters and prevent penetration thereinto by biasing means such as wavy bias or leaf springs 51. Springs 51, as best illustrated in FIG. 2, are disposed between insulation 50 and spacers 49 to urge the electric heaters against the bottoms of their slots. Spring 51 for urging heater 34 was deleted for purposes of clarity. Biasing means such as springs or Bellville washers 52 are disposed in cooperating indentations 54 and 56 formed on circumferentially adjacent ends of foundation members 24 and 26 respectively. Indentations 54 and 56 restrain springs 52 within a relatively small radial distance as illustrated in FIG. 3 and a relatively small axial distance as illustrated in FIG. 2. Springs 52 and 54 permit the shaft bore heater assembly to be inserted and removed from shaft 16 with relative ease while maintaining good heat transfer contact between inner shaft surface 16b and both outer surfaces 58 and 60 of foundation members 24 and 26, respectively, during relatively slow shaft rotation or rest.
FIG. 2 is a partial transverse sectional view of electrical input generator flange 12 and its connection with heaters 34 and 40. For comparative purposes heaters 40 and 34 are illustrated in their non-heating and heating positions respectively. As can be seen, heater 34 is elongated in the axial direction due to thermal expansion from heat generated by that heater. Double rings 62, 64, 66, 68, 70, and 72 are illustrated along the outer periphery of flange 12. Conducting studs extending radially through flange 12 from inner rings 64, 68, and 72 provide electrical energy through flexible or braided connectors to the electrical heaters which constitute a portion of the present invention. The details of such double slip-ring construction are set forth in copending application Ser. No. 857,480, filed Dec. 5, 1977.
For illustrative purposes here, only copper stud 74 connecting slip ring pair 62 and 64 is shown in operating position providing electrical energy to heater 40 through flexible or braided conducting connector 76. Each pair of slip rings is connected to two heaters. The preferred embodiment has three-phase power supplied to the illustrated six heaters which are wired in delta.
Although delta wiring from a three-phase power supply to six electrical heaters has been indicated as preferred, it is to be understood that any number of electrical heaters may be utilized with any comparable single or multiphase power supply system and those heaters may be electrically wired in "Y" as well. Furthermore, any number of heater foundation members may be utilized to form the preferred, assembled cylindrical shape since the invention is not to be limited to dual semi-cylindrical foundation members.
It will now be apparent that an improved apparatus for heating turbine shaft bores has been provided in which electrical heaters are utilized to heat the turbine shaft from the inside so as to reduce thermal shock on the shaft from inlet steam at initiation of turbine operation and thus permit shorter turbine startup times due to greater allowable rotative acceleration rates. Furthermore, the turbine shaft bore heater assembly results in a mechanical stable structure whose life is substantially the same as the turbine's and whose failure will not adversely affect the turbine's start up time over those of prior startup methods. Such rapid startups permit better generating response to load demand and decrease the high cost sustained in present, lengthy turbine startups.

Claims (9)

We claim:
1. A shaft bore heater assembly comprising:
a hollow, heat conductive rotatable shaft having an inside and an outside surface;
a plurality of heater foundation members having inner and outer surfaces, at least a portion of said outer surfaces being engageable with said shaft's inside surface, said members having open-mount slots in one of said surfaces, said slots having bottoms;
a plurality of electrical heaters insertable in said slots, said electrical heaters being electrically interconnected and having electrical leads at least at one axial end, said heaters being electrically insulated from said foundation members;
means for restraining said heaters in said slots; and
means for biasing said foundation members' outer surfaces into engagement with said shaft's inside surface.
2. The shaft bore heater assembly of claim 1 wherein said foundation members are arcuate portions of a substantially cylindrical structure which obtains when said foundation members are assembled in operating position.
3. The shaft bore heater assembly of claim 2 wherein said biasing means are disposed between the circumferentially adjacent heater foundation members.
4. The shaft bore heater assembly of claim 3 wherein said biasing means are restrained in biasing position by disposing portions of said biasing means in indentations formed on the circumferential ends of the circumferentially adjacent foundation members.
5. The shaft bore heater assembly of claim 1 wherein said slots are equally spaced in the circumferential direction and axially disposed.
6. The shaft bore heater assembly of claim 1, said restraining means comprising:
means for covering the open mouths of said slots; and
means for biasing said electrical heaters away from said covering means against the slots' bottoms.
7. The shaft bore heater assembly of claim 6, said covering means comprising:
insulation disposed on and attached to said surface in which said slots' open-mouths are exposed.
8. The shaft bore heater assembly of claim 6, said electrical heater biasing means comprising:
a plurality of spring members disposed between said electrical heaters and said covering means.
9. The shaft bore heater assembly of claim 6 further comprising:
a plurality of rigid spacer members disposed in said slots between and engageable with said electrical heaters and said heater biasing means.
US05/857,481 1977-12-05 1977-12-05 Hollow shaft bore heater assembly Expired - Lifetime US4200784A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US05/857,481 US4200784A (en) 1977-12-05 1977-12-05 Hollow shaft bore heater assembly
IT30255/78A IT1100599B (en) 1977-12-05 1978-11-28 HOLE SHAFT HEATING COMPLEX
JP14975478A JPS5486828A (en) 1977-12-05 1978-12-05 Device for heating inside surface of shaft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/857,481 US4200784A (en) 1977-12-05 1977-12-05 Hollow shaft bore heater assembly

Publications (1)

Publication Number Publication Date
US4200784A true US4200784A (en) 1980-04-29

Family

ID=25326087

Family Applications (1)

Application Number Title Priority Date Filing Date
US05/857,481 Expired - Lifetime US4200784A (en) 1977-12-05 1977-12-05 Hollow shaft bore heater assembly

Country Status (3)

Country Link
US (1) US4200784A (en)
JP (1) JPS5486828A (en)
IT (1) IT1100599B (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4329566A (en) * 1980-12-12 1982-05-11 Pitney Bowes Inc. Heated fuser roll
US5451258A (en) * 1994-05-11 1995-09-19 Materials Research Corporation Apparatus and method for improved delivery of vaporized reactant gases to a reaction chamber
EP1739285A1 (en) * 2005-07-01 2007-01-03 Siemens Aktiengesellschaft Cooled gas turbine stator vane and method of operation of a gas turbine
US20090325000A1 (en) * 2008-06-25 2009-12-31 Ford Motor Company Automotive rotatable power transfer system and method of operating same
US20110167820A1 (en) * 2010-01-12 2011-07-14 Mikael Fredriksson Heating system for a turbine
US20120187108A1 (en) * 2009-02-12 2012-07-26 Rainer Schwarz Assembly, device and method for attaching a contact tube to a shaft of a continuous resistance annealer for wires
US8454340B1 (en) * 2008-03-25 2013-06-04 Radyne Corporation Heat treated formation of tubular articles
CN103267636A (en) * 2013-05-10 2013-08-28 西安航空动力股份有限公司 Heating device for aero-engine spindle thermal state strength test
US9903374B2 (en) 2012-12-21 2018-02-27 Nuovo Pignone Srl Multistage compressor and method for operating a multistage compressor

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1811383A (en) * 1928-05-03 1931-06-23 Bbc Brown Boveri & Cie Means for preheating turbines
US2004777A (en) * 1933-05-27 1935-06-11 Gen Electric Elastic fluid turbine
US2874257A (en) * 1952-08-27 1959-02-17 Cutler Hammer Inc Electrical resistor units
US2875312A (en) * 1956-09-27 1959-02-24 Thermel Inc Heating assembly and method of production thereof
US3151633A (en) * 1961-03-29 1964-10-06 Owens Corning Fiberglass Corp Shaped thermal insulation for pipe
US3484581A (en) * 1964-01-22 1969-12-16 Whitin Machine Works Godet roll
US3720808A (en) * 1971-11-08 1973-03-13 Gen Binding Corp Ceramic core laminating roll
US3997758A (en) * 1974-03-14 1976-12-14 Westinghouse Electric Corporation Moisture control device for steam turbines

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1811383A (en) * 1928-05-03 1931-06-23 Bbc Brown Boveri & Cie Means for preheating turbines
US2004777A (en) * 1933-05-27 1935-06-11 Gen Electric Elastic fluid turbine
US2874257A (en) * 1952-08-27 1959-02-17 Cutler Hammer Inc Electrical resistor units
US2875312A (en) * 1956-09-27 1959-02-24 Thermel Inc Heating assembly and method of production thereof
US3151633A (en) * 1961-03-29 1964-10-06 Owens Corning Fiberglass Corp Shaped thermal insulation for pipe
US3484581A (en) * 1964-01-22 1969-12-16 Whitin Machine Works Godet roll
US3720808A (en) * 1971-11-08 1973-03-13 Gen Binding Corp Ceramic core laminating roll
US3997758A (en) * 1974-03-14 1976-12-14 Westinghouse Electric Corporation Moisture control device for steam turbines

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4329566A (en) * 1980-12-12 1982-05-11 Pitney Bowes Inc. Heated fuser roll
US5451258A (en) * 1994-05-11 1995-09-19 Materials Research Corporation Apparatus and method for improved delivery of vaporized reactant gases to a reaction chamber
EP1739285A1 (en) * 2005-07-01 2007-01-03 Siemens Aktiengesellschaft Cooled gas turbine stator vane and method of operation of a gas turbine
US20070116563A1 (en) * 2005-07-01 2007-05-24 Fathi Ahmad Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine
US7465150B2 (en) 2005-07-01 2008-12-16 Siemens Aktiengesellachaft Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine
US20090074572A1 (en) * 2005-07-01 2009-03-19 Fathi Ahmad Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine
US8454340B1 (en) * 2008-03-25 2013-06-04 Radyne Corporation Heat treated formation of tubular articles
US20090325000A1 (en) * 2008-06-25 2009-12-31 Ford Motor Company Automotive rotatable power transfer system and method of operating same
US9496569B2 (en) 2008-06-25 2016-11-15 Ford Motor Company Automotive rotatable power transfer system and method of operating same
US20120187108A1 (en) * 2009-02-12 2012-07-26 Rainer Schwarz Assembly, device and method for attaching a contact tube to a shaft of a continuous resistance annealer for wires
US20110167820A1 (en) * 2010-01-12 2011-07-14 Mikael Fredriksson Heating system for a turbine
US8695342B2 (en) * 2010-01-12 2014-04-15 Siemens Aktiengesellschaft Heating system for a turbine
US9903374B2 (en) 2012-12-21 2018-02-27 Nuovo Pignone Srl Multistage compressor and method for operating a multistage compressor
CN103267636A (en) * 2013-05-10 2013-08-28 西安航空动力股份有限公司 Heating device for aero-engine spindle thermal state strength test
CN103267636B (en) * 2013-05-10 2015-10-28 西安航空动力股份有限公司 For the heating arrangement of aero-engine spindle thermal state strength test

Also Published As

Publication number Publication date
JPS5486828A (en) 1979-07-10
IT7830255A0 (en) 1978-11-28
JPS5520052B2 (en) 1980-05-30
IT1100599B (en) 1985-09-28

Similar Documents

Publication Publication Date Title
US7112036B2 (en) Rotor and bearing system for a turbomachine
US4200784A (en) Hollow shaft bore heater assembly
US3950950A (en) Rotary Rankine engine powered electric generating apparatus
US3733502A (en) Liquid cooled rotor for dynamoelectric machines
US3430441A (en) Engine for converting energy by thermal expansion of solids
JPS63228934A (en) Rotor for rotary electric machine
JP3529137B2 (en) A power generation unit having a combined cycle and including a gas turbine and a steam turbine having a plurality of modules
US4453101A (en) Amortisseur bar with improved interface between free conductor bars and amortisseur ring
US3872335A (en) Rotating rectifier assembly for brushless exciters
RU2717565C1 (en) Synchronous generator of gearless wind-driven power plant, as well as method for manufacturing synchronous generator and use of template windings
BR112017021933B1 (en) ROTATING DYNAMOELECTRIC MACHINE, WIND POWER GENERATOR, AND WIND POWER INSTALLATION
US4341968A (en) Support means for high-temperature generator stators
US5068564A (en) End retainer ring assembly for rotary electrical devices
US3916230A (en) Liquid-cooled rotor for dynamoelectric machines
US4658170A (en) Rotor for a superconducting rotating electric machine
US20130147310A1 (en) Slip ring
US4047063A (en) Liquid metal slip-ring arrangement for a dynamo electric machine
WO2013143872A1 (en) A system for inductive heating of turbine rotor disks
US4237392A (en) Rotor member for a superconducting generator
JP2709403B2 (en) Rotary electric machine
US4439701A (en) Rotor of a superconductive rotary electric machine
US4180300A (en) Double ring and radial conductor assembly for large hollow shafts
US3868520A (en) Turbine-generator water-cooled rotor shaft liner restraint
SU609494A3 (en) Electric machine
KR20130108374A (en) Rotor for an electric machine